FieldKeplerianOrbit

ElementMissed InstructionsCov.Missed BranchesCov.MissedCxtyMissedLinesMissedMethods
Total15 of 4,43899%4 of 11896%41273595065
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)1024296%22090%21425201
addKeplerContribution(PositionAngleType, CalculusFieldElement, CalculusFieldElement[])11995%1375%1411501
computeJacobianMeanWrtCartesianElliptical()778100%n/a0108601
computeJacobianMeanWrtCartesianHyperbolic()749100%n/a0108901
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement, boolean)470100%6100%0406001
computePVWithoutA()218100%4100%0302801
nonKeplerianAcceleration()203100%n/a0102201
FieldKeplerianOrbit(Field, KeplerianOrbit)133100%12100%0701101
initPosition()118100%2100%0201401
shiftedBy(CalculusFieldElement)114100%2100%0201701
referenceAxes()111100%n/a0101701
computeJacobianTrueWrtCartesianElliptical()89100%2100%0201301
computeJacobianTrueWrtCartesianHyperbolic()88100%2100%0201501
toOrbit()83100%2100%020901
computeJacobianEccentricWrtCartesianHyperbolic()58100%2100%0201001
computeJacobianEccentricWrtCartesianElliptical()57100%2100%020801
toString()51100%n/a010801
getHxDot()49100%4100%030701
getHyDot()49100%4100%030701
initPVCoordinates()49100%2100%020701
getEccentricAnomalyDot()41100%4100%030801
getMeanAnomalyDot()41100%4100%030801
getEquinoctialExDot()38100%2100%020601
getEquinoctialEyDot()38100%2100%020601
checkParameterRangeInclusive(String, double, double, double)35100%1375%130401
getHx()31100%2100%020301
getHy()31100%2100%020301
removeRates()27100%n/a010301
FieldKeplerianOrbit(CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, CalculusFieldElement, PositionAngleType, Frame, FieldAbsoluteDate, CalculusFieldElement)19100%n/a010201
getEccentricAnomaly()18100%2100%020301
getMeanAnomaly()18100%2100%020301
getLvDot()16100%2100%020201
getLEDot()16100%2100%020201
getLMDot()16100%2100%020201
getAnomaly(PositionAngleType)15100%4100%030301
getAnomalyDot(PositionAngleType)15100%4100%030301
getEquinoctialEx()12100%n/a010101
getEquinoctialEy()12100%n/a010101
FieldKeplerianOrbit(FieldOrbit)11100%n/a010201
getLv()11100%n/a010101
getLE()11100%n/a010101
getLM()11100%n/a010101
FieldKeplerianOrbit(FieldPVCoordinates, Frame, FieldAbsoluteDate, CalculusFieldElement)10100%n/a010201
FieldKeplerianOrbit(TimeStampedFieldPVCoordinates, Frame, CalculusFieldElement)9100%n/a010201
computeJacobianMeanWrtCartesian()9100%2100%020301
computeJacobianEccentricWrtCartesian()9100%2100%020301
computeJacobianTrueWrtCartesian()9100%2100%020301
FieldKeplerianOrbit(Field, Orbit)8100%n/a010201
shiftedBy(double)8100%n/a010101
hasDerivatives()7100%2100%020101
getA()100%n/a010101
getADot()100%n/a010101
getE()100%n/a010101
getEDot()100%n/a010101
getI()100%n/a010101
getIDot()100%n/a010101
getPerigeeArgument()100%n/a010101
getPerigeeArgumentDot()100%n/a010101
getRightAscensionOfAscendingNode()100%n/a010101
getRightAscensionOfAscendingNodeDot()100%n/a010101
getTrueAnomaly()100%n/a010101
getTrueAnomalyDot()100%n/a010101
hasRates()100%n/a010101
getType()100%n/a010101
getCachedPositionAngleType()100%n/a010101